Flow stability model for fan/compressors with annular duct and novel casing treatment

Chinese Journal of Aeronautics

Volumn 25, Issue 2, 2012, Pages 143-154

  Liu, Xiaohua ^a   Sun, Dakun ^a   Sun, Xiaofeng ^a   Wang, Xiaoyu ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

casing treatment; compressor; eigenvalue; rotating stall; stability

Indexed keywords

AXIAL FLOW FAN; BACKCHAMBER; CASING TREATMENT; COMPLEX FREQUENCY; DIFFERENT BOUNDARY CONDITION; EFFICIENCY LOSS; EIGEN-VALUE; EIGENVALUES; EXPERIMENTAL INVESTIGATIONS; FLOW STABILITY; HOMOGENEOUS EQUATIONS; IMAGINARY PARTS; MULTI-STAGE; NUMERICAL EVALUATIONS; OPEN AREA RATIO; ROTATING STALLS; STABILITY EQUATIONS; STABILITY MODELS; STALL INCEPTION; STALL MARGIN; UNSTEADY PHENOMENA; WALL IMPEDANCE;

ANNULAR DUCTS; AXIAL FLOW; COMPRESSORS; CONVERGENCE OF NUMERICAL METHODS; EIGENVALUES AND EIGENFUNCTIONS; PERFORATED PLATES; STABILITY;

THREE DIMENSIONAL;

EID: 84860452445     PISSN: 10009361     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1000-9361(11)60373-7     Document Type: Article

References (38)

1. Emmons HW, Pearson CE, Grant HP Compressor surge and stall propagation Transactions of the ASME 79 4 1955 455 469
2. Nenni JP, Ludwig GR. A theory to predict the inception of rotating stall in axial flow compressors. AIAA-1974-528, 1974.
3. Ludwig GR, Nenni JP. Basic studies of rotating stall in axial flow compressors. AFAPL-TR-79-2083, 1979.
4. Stenning AH Rotating stall and surge Journal of Fluids Engineering 102 1 1980 14 20
5. Sun XF. On the relation between the inception of rotating stall and casing treatment. AIAA-1996-2579, 1996.
6. Sun XF, Sun DK, Yu WW A model to predict stall inception of transonic axial flow fan/compressors Chinese Journal of Aeronautics 24 6 2011 687 700
7. AJ Crook, EM Greitzer, CS Tan et al. Numerical simulation of compressor endwall and casing treatment flow phenomena Journal of Turbomachinery 115 3 1993 501 511
8. Gorrel SE, Russler PM. Stall inception in a high-speed low aspect ratio fan including the effects of casing treatments. ASME-GT-332, 1994.
9. Kang CS, Mckenzie AB, Elder RL. Recessed casing treatment effects on fan performance and flow field. ASME-GT-197, 1995.
10. Bard H Fan stability by anti-stall in tunnels and industrial process ventilation, turbo compressor and fan stability 1993 Fluid Machinery Committee of Institution of Mechanical Engineer
11. Azimian AR, Elder RL, McKenzie AB Application of recess vaned casing treatment to axial flow fan Journal of Turbomacinery 112 1 1990 145 150 (Pubitemid 20646720)
12. Ziabasharhagh M, McKenzie AB, Elder RL. Recess vane passive stall control. ASME-GT-36, 1992.
13. Paduano JD, Greitzer EM, Epstein AH Compression system stability and active control Annual Review of Fluid Mechanics 33 2001 491 517
14. CS Tan, I Day, S Morris et al. Spike-type compressor stall inception, detection, and control Annual Review of Fluid Mechanics 42 2010 275 300
15. Osborn WM, Lewis GW, Heidelberg LJ. Effect of several porous casing treatments on stall limit and on overall performance of axial-flow compressor rotor. NASA TN D-6537, 1971.
16. Osborn WM, Moore RD. Effect of casing treatment on overall performance of axial-flow transonic fan stage with pressure ratio of 1.75 and tip solidity of 1.5. NASA TM X-3477, 1977.
17. Takata H, Tsukuda Y Stall margin improvement by casing treatment - its mechanism and effectiveness ASME Journal of Engineering for Power 99 1979 121 133
18. EM Greitzer, JP Nikkanen, DE Haddad et al. A fundamental criterion for the application of rotor casing treatment Journal of Fluid Engineering 101 2 1979 237 243 (Pubitemid 10411206)
19. Smith GDJ, Cumpsty NA Flow phenomena in compressor casing treatment Journal of Engineering for Gas Turbines and Powers 106 1984 533 541
20. Sun DK, Hou RW, Sun XF An experimental investigation of rotating stall margin improvement with unsteady casing treatments Journal of Aerospace Power 23 4 2008 662 670 [in Chinese].
21. Sun DK, Sun XF An experimental study on inhibition of unsteady casing treatment on stall inception Journal of Aerospace Power 23 4 2008 671 679 [in Chinese].
22. Brazier-Smith PR, Scott JF On the determination of the dispersion equations by use of winding number integrals Journal of Sound and Vibration 145 3 1991 503 510
23. Ivansson S, Karasalo I Computation of modal numbers using an adaptive winding-number integral method with error control Journal of Sound and Vibration 161 1 1993 173 180 (Pubitemid 23631744)
24. Bechert DW Sound absorption caused by vorticity shedding, demonstrated with a jet flow Journal of Sound and Vibration 70 3 1980 389 405 (Pubitemid 11441506)
25. Howe MS Theory of vortex sound 2002 Cambridge University Press Cambridge
26. Howe MS. On the theory of unsteady high Reynolds number flow through a circular aperture. Proceedings of the Royal Society London A366. 1979; 205-223. (Pubitemid 9456689)
27. Jing XD, Sun XF Wall thickness influence on the impedance of perforated plates with bias flow AIAA Journal 38 9 2000 1573 1578
28. Jing XD, Sun XF Sound-excited flow and acoustic nonlinearity at an orifice Physics of Fluids 14 1 2002 268 276
29. XD Jing, XF Sun, J Wu et al. Effect of grazing flow on the acoustic impedance of an orifice AIAA Journal 39 8 2001 1478 1484 (Pubitemid 32749830)
30. XF Sun, XD Jing, H Zhang et al. Effect of grazing-bias flow interaction on acoustic impedance of perforated plates Journal of Sound and Vibration 254 3 2002 557 573 (Pubitemid 35275031)
31. Peat KS, Ih JG, Lee SH The acoustic impedance of a circular orifice in grazing mean flow: comparison with theory Journal of the Acoustical Society of America 114 6 2003 3076 3086 (Pubitemid 37553621)
32. Namba M, Fukushige K Application of the equivalent surface source method to the acoustics of duct systems with non-uniform wall impedance Journal of Sound and Vibration 73 1 1980 125 146 (Pubitemid 11477428)
33. XF Sun, XY Wang, L Du et al. A new model for the prediction of turbofan noise with the effect of locally and non-locally reacting liners Journal of Sound and Vibration 316 1-5 2008 50 68
34. Moore RD, Reid L. Performance of single-stage axial flow transonic compressor with rotor and stator aspect ratios of 1.19 and 1.26, respectively, and with design pressure ratio of 2.05. NASA TP-2001, 1980.
35. M Tryfonidis, O Etchevers, JD Paduano et al. Pre-stall behavior of several high-speed compressors Journal of Turbomachinery 117 1 1995 62 80
36. Weigl HJ Active stabilization of rotating stall and surge in a transonic single-stage axial compressor Journal of Turbomachinery 120 4 1998 625 636 (Pubitemid 29139723)
37. Greitzer EM, Moore FK A theory of post-stall transients in axial compression systems: part I - development of equations Journal of Engineering for Gas Turbine and Power 108 1 1986 68 76 (Pubitemid 16475797)
38. Greitzer EM, Moore FK A theory of post-stall transients in axial compression systems: part II - application Journal of Engineering for Gas Turbine and Power 108 2 1986 231 239 (Pubitemid 16533469)